Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps:
Gespeichert in:
Hauptverfasser: | , |
---|---|
Format: | Buch |
Sprache: | Undetermined |
Veröffentlicht: |
Washington
NACA
1949
|
Schriftenreihe: | United States / National Advisory Committee for Aeronautics: Report
942 |
Beschreibung: | 23 S graph. Darst. |
Internformat
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100 | 1 | |a Sivells, James C. |e Verfasser |4 aut | |
245 | 1 | 0 | |a Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps |c by James C. Sivells and Stanley H. Spooner |
264 | 1 | |a Washington |b NACA |c 1949 | |
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490 | 1 | |a United States / National Advisory Committee for Aeronautics: Report |v 942 | |
700 | 1 | |a Spooner, Stanley H. |e Verfasser |4 aut | |
810 | 2 | |a National Advisory Committee for Aeronautics: Report |t United States |v 942 |w (DE-604)BV008910189 |9 942 | |
999 | |a oai:aleph.bib-bvb.de:BVB01-008770795 |
Datensatz im Suchindex
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any_adam_object | |
author | Sivells, James C. Spooner, Stanley H. |
author_facet | Sivells, James C. Spooner, Stanley H. |
author_role | aut aut |
author_sort | Sivells, James C. |
author_variant | j c s jc jcs s h s sh shs |
building | Verbundindex |
bvnumber | BV012884457 |
ctrlnum | (DE-599)BVBBV012884457 |
format | Book |
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id | DE-604.BV012884457 |
illustrated | Illustrated |
indexdate | 2024-07-09T18:35:28Z |
institution | BVB |
language | Undetermined |
oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-008770795 |
open_access_boolean | |
physical | 23 S graph. Darst. |
publishDate | 1949 |
publishDateSearch | 1949 |
publishDateSort | 1949 |
publisher | NACA |
record_format | marc |
series2 | United States / National Advisory Committee for Aeronautics: Report |
spelling | Sivells, James C. Verfasser aut Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps by James C. Sivells and Stanley H. Spooner Washington NACA 1949 23 S graph. Darst. txt rdacontent n rdamedia nc rdacarrier United States / National Advisory Committee for Aeronautics: Report 942 Spooner, Stanley H. Verfasser aut National Advisory Committee for Aeronautics: Report United States 942 (DE-604)BV008910189 942 |
spellingShingle | Sivells, James C. Spooner, Stanley H. Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps |
title | Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps |
title_auth | Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps |
title_exact_search | Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps |
title_full | Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps by James C. Sivells and Stanley H. Spooner |
title_fullStr | Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps by James C. Sivells and Stanley H. Spooner |
title_full_unstemmed | Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps by James C. Sivells and Stanley H. Spooner |
title_short | Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps |
title_sort | investigation in the langley 19 foot pressure tunnel of two wings of naca 65 210 and 64 210 airfoil sections with various type flaps |
volume_link | (DE-604)BV008910189 |
work_keys_str_mv | AT sivellsjamesc investigationinthelangley19footpressuretunneloftwowingsofnaca65210and64210airfoilsectionswithvarioustypeflaps AT spoonerstanleyh investigationinthelangley19footpressuretunneloftwowingsofnaca65210and64210airfoilsectionswithvarioustypeflaps |